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DE60229022D1 - Method and apparatus for cooling pilot burners in gas turbines - Google Patents

Method and apparatus for cooling pilot burners in gas turbines

Info

Publication number
DE60229022D1
DE60229022D1 DE60229022T DE60229022T DE60229022D1 DE 60229022 D1 DE60229022 D1 DE 60229022D1 DE 60229022 T DE60229022 T DE 60229022T DE 60229022 T DE60229022 T DE 60229022T DE 60229022 D1 DE60229022 D1 DE 60229022D1
Authority
DE
Germany
Prior art keywords
gas turbines
pilot burners
cooling pilot
cooling
burners
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
DE60229022T
Other languages
German (de)
Inventor
Gilbert Farmer
Ella Christine Kutter
Steven Clayton Vise
John Robert Staker
Marwan Al-Roub
Tariq Kay Harris
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of DE60229022D1 publication Critical patent/DE60229022D1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00012—Details of sealing devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03044—Impingement cooled combustion chamber walls or subassemblies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE60229022T 2001-05-17 2002-05-15 Method and apparatus for cooling pilot burners in gas turbines Expired - Lifetime DE60229022D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/859,611 US6557350B2 (en) 2001-05-17 2001-05-17 Method and apparatus for cooling gas turbine engine igniter tubes

Publications (1)

Publication Number Publication Date
DE60229022D1 true DE60229022D1 (en) 2008-11-06

Family

ID=25331325

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60229022T Expired - Lifetime DE60229022D1 (en) 2001-05-17 2002-05-15 Method and apparatus for cooling pilot burners in gas turbines

Country Status (4)

Country Link
US (1) US6557350B2 (en)
EP (1) EP1258682B1 (en)
JP (1) JP4128393B2 (en)
DE (1) DE60229022D1 (en)

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US6715279B2 (en) * 2002-03-04 2004-04-06 General Electric Company Apparatus for positioning an igniter within a liner port of a gas turbine engine
GB0227842D0 (en) * 2002-11-29 2003-01-08 Rolls Royce Plc Sealing Arrangement
US20040268393A1 (en) * 2003-05-08 2004-12-30 Hunleth Frank A. Control framework with a zoomable graphical user interface for organizing, selecting and launching media items
US8601396B2 (en) * 2003-05-08 2013-12-03 Hillcrest Laboratories, Inc. Systems and methods for node tracking and notification in a control framework including a zoomable graphical user interface
US8555165B2 (en) * 2003-05-08 2013-10-08 Hillcrest Laboratories, Inc. Methods and systems for generating a zoomable graphical user interface
US8046705B2 (en) * 2003-05-08 2011-10-25 Hillcrest Laboratories, Inc. Systems and methods for resolution consistent semantic zooming
FR2856466B1 (en) * 2003-06-20 2005-08-26 Snecma Moteurs APPARATUS FOR SEALING NON-WELDED CANDLE ON CHAMBER WALL
WO2005109879A2 (en) 2004-04-30 2005-11-17 Hillcrest Laboratories, Inc. Free space pointing devices and method
US8629836B2 (en) 2004-04-30 2014-01-14 Hillcrest Laboratories, Inc. 3D pointing devices with orientation compensation and improved usability
US7299620B2 (en) * 2004-06-29 2007-11-27 Peter Stuttaford Tornado torch igniter
WO2006058129A2 (en) 2004-11-23 2006-06-01 Hillcrest Laboratories, Inc. Semantic gaming and application transformation
US7546739B2 (en) * 2005-07-05 2009-06-16 General Electric Company Igniter tube and method of assembling same
FR2891350A1 (en) * 2005-09-29 2007-03-30 Snecma Sa DEVICE FOR GUIDING AN ELEMENT IN AN ORIFICE OF A TURBOMACHINE COMBUSTION CHAMBER WALL
US7926279B2 (en) * 2006-09-21 2011-04-19 Siemens Energy, Inc. Extended life fuel nozzle
US8479490B2 (en) * 2007-03-30 2013-07-09 Honeywell International Inc. Combustors with impingement cooled igniters and igniter tubes for improved cooling of igniters
US20090293486A1 (en) * 2007-10-26 2009-12-03 Honeywell International, Inc. Combustors with igniters having protrusions
FR2925147B1 (en) * 2007-12-14 2012-07-13 Snecma DEVICE FOR GUIDING AN ELEMENT IN AN ORIFICE OF A TURBOMACHINE COMBUSTION CHAMBER WALL
FR2927367B1 (en) * 2008-02-11 2010-05-28 Snecma DEVICE FOR MOUNTING AN IGNITION CANDLE IN A GAS TURBINE ENGINE COMBUSTION CHAMBER
US8046987B2 (en) * 2008-09-03 2011-11-01 Woodard, Inc. Air cooled core mounted ignition system
US20100212324A1 (en) * 2009-02-26 2010-08-26 Honeywell International Inc. Dual walled combustors with impingement cooled igniters
FR2952698B1 (en) * 2009-11-17 2013-09-20 Snecma COMBUSTION CHAMBER WITH VENTILATED SPARK PLUG
FR2952703B1 (en) 2009-11-19 2011-10-28 Snecma GUIDE TO AN IGNITION CANDLE IN A COMBUSTION CHAMBER OF A TURBOMACHINE
US8726631B2 (en) * 2009-11-23 2014-05-20 Honeywell International Inc. Dual walled combustors with impingement cooled igniters
US9157638B2 (en) * 2012-01-31 2015-10-13 General Electric Company Adaptor assembly for removable components
JP5924618B2 (en) * 2012-06-07 2016-05-25 川崎重工業株式会社 Fuel injection device
US9249978B2 (en) * 2012-07-03 2016-02-02 Alstom Technology Ltd Retaining collar for a gas turbine combustion liner
US9228747B2 (en) 2013-03-12 2016-01-05 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
WO2014168654A1 (en) 2013-03-14 2014-10-16 Rolls-Royce Corporation Inverted cap igniter tube
US9989254B2 (en) * 2013-06-03 2018-06-05 General Electric Company Combustor leakage control system
US9803554B2 (en) 2013-08-12 2017-10-31 Unison Industries, Llc Fuel igniter assembly having heat-dissipating element and methods of using same
DE102013222932A1 (en) * 2013-11-11 2015-05-28 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustion chamber with shingle for carrying out a spark plug
US10156189B2 (en) * 2014-01-28 2018-12-18 Pratt & Whitney Canada Corp. Combustor igniter assembly
US20160047317A1 (en) * 2014-08-14 2016-02-18 General Electric Company Fuel injector assemblies in combustion turbine engines
US10612781B2 (en) * 2014-11-07 2020-04-07 United Technologies Corporation Combustor wall aperture body with cooling circuit
US20170176004A1 (en) * 2015-12-18 2017-06-22 Pratt & Whitney Canada Corp. Combustor floating collar assembly
US20180030899A1 (en) * 2016-07-27 2018-02-01 Honda Motor Co., Ltd. Structure for supporting spark plug for gas turbine engine
FR3081211B1 (en) * 2018-05-16 2021-02-26 Safran Aircraft Engines TURBOMACHINE COMBUSTION CHAMBER SET
US11286861B2 (en) 2018-09-12 2022-03-29 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11415060B2 (en) 2018-09-12 2022-08-16 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11454173B2 (en) 2018-09-12 2022-09-27 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11391213B2 (en) 2018-09-12 2022-07-19 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11255271B2 (en) 2018-09-12 2022-02-22 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11268447B2 (en) 2018-09-12 2022-03-08 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11268486B2 (en) 2018-09-12 2022-03-08 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11391212B2 (en) 2018-09-12 2022-07-19 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11408351B2 (en) 2018-09-12 2022-08-09 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11401867B2 (en) 2018-09-12 2022-08-02 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
FR3096114B1 (en) * 2019-05-13 2022-10-28 Safran Aircraft Engines Combustion chamber comprising means for cooling an annular envelope zone downstream of a stack
US11187152B1 (en) 2020-09-30 2021-11-30 General Electric Company Turbomachine sealing arrangement having a cooling flow director
US11702991B2 (en) 2020-09-30 2023-07-18 General Electric Company Turbomachine sealing arrangement having a heat shield
US11859819B2 (en) 2021-10-15 2024-01-02 General Electric Company Ceramic composite combustor dome and liners

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US2422213A (en) * 1944-06-09 1947-06-17 Westinghouse Electric Corp Combustion chamber
CA992755A (en) * 1972-10-02 1976-07-13 General Electric Company Gas turbine engine igniter assembly
US4194358A (en) 1977-12-15 1980-03-25 General Electric Company Double annular combustor configuration
US4628694A (en) * 1983-12-19 1986-12-16 General Electric Company Fabricated liner article and method
US4875339A (en) * 1987-11-27 1989-10-24 General Electric Company Combustion chamber liner insert
US5088287A (en) 1989-07-13 1992-02-18 Sundstrand Corporation Combustor for a turbine
US5129231A (en) * 1990-03-12 1992-07-14 United Technologies Corporation Cooled combustor dome heatshield
US5402637A (en) 1993-07-13 1995-04-04 Cooper Industries Igniter plug extender for a turbine engine combustor
US5442907A (en) * 1994-04-04 1995-08-22 Aero-Plasma, Inc. Bootstrap re-ignition system for aircraft jet engine
US6212870B1 (en) 1998-09-22 2001-04-10 General Electric Company Self fixturing combustor dome assembly
US6266961B1 (en) * 1999-10-14 2001-07-31 General Electric Company Film cooled combustor liner and method of making the same
US6438958B1 (en) * 2000-02-28 2002-08-27 General Electric Company Apparatus for reducing heat load in combustor panels

Also Published As

Publication number Publication date
JP2002364848A (en) 2002-12-18
EP1258682A2 (en) 2002-11-20
US20020170293A1 (en) 2002-11-21
JP4128393B2 (en) 2008-07-30
US6557350B2 (en) 2003-05-06
EP1258682B1 (en) 2008-09-24
EP1258682A3 (en) 2004-01-21

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition